View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 39440U 26135.30373852 +.00000000 +00000-0 +14843-3 0 00004
2 39440 97.8895 84.1550 0058982 135.2304 225.3698 14.93498377 01
| Epoch (UTC): | 15 May 2026 07:17:23 |
| Eccentricity: | 0.0058982 |
| inclination: | 97.8895° |
| perigee height: | 546 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 84.1550° |
| argument of perigee: | 135.2304° |
| revolutions per day: | 14.93498377 |
| mean anomaly at epoch: | 225.3698° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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